Consideration of airplane wheel brakes and indication of probable improvements; at least half of increased weight of braked undercarriage is directly due to heavier structure required for transmitting torque loads; essential requirements of braked under-carriages; separate control to each wheel; writer does not think that any servo-motor carried apart from wheel should be considered; particulars of Bendix self-energizing brake unit; points to watch in wheel mounting.
Wheel brake equipment for aircraft
Aeroplane
Aeroplane ; 35 , n 9
1928
2 pages
5 Figs.
Aufsatz (Zeitschrift)
Englisch
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